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US2600715A - Hydraulic brake actuator for helicopter rotors - Google Patents

Hydraulic brake actuator for helicopter rotors Download PDF

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US2600715A
US2600715A US136445A US13644550A US2600715A US 2600715 A US2600715 A US 2600715A US 136445 A US136445 A US 136445A US 13644550 A US13644550 A US 13644550A US 2600715 A US2600715 A US 2600715A
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reservoir
fluid
hydraulic
chamber
actuator
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US136445A
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John W Wheeler
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Bell Aircraft Corp
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Bell Aircraft Corp
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/32Rotors
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/04Helicopters
    • B64C27/12Rotor drives

Definitions

  • Thisinvention relates to helicopter aircraft, and more particularly to an improved hydraulic brake device for helicopter rotors and the like wherein the brake actuator mechanism is necessarily at a higher elevation than the control piston-cylinder mechanism.
  • Another object of the invention is to provide an improved braking system of the character aforesaid which automatically maintains a predetermined constant pressure differential in the braking system relative to the ambient atmosphere in spite of variations in the atmospheric pressure.
  • Another object of the invention is to provide an improved braking system of the character aforesaid which operates automatically to maintain the hydraulic line between the control piston and the brake actuator filled with hydraulic fluid and to prevent cavitation therein, whereby pumping of the control piston is unnecessary to condition the system for effective operation, and whereby uniformly short stroke operation of the control piston will provide effective brake actuation.
  • Another object of the invention is to provide an improved braking system embodying the features aforesaid and which is of relatively simple and inexpensive yet rugged construction.
  • Fig. 1 is a fragmentary side elevation of a helicopter aircraft embodying a rotor brake system of the invention
  • Fig. 2 is a fragmentary vertical section throug the manual control portion of the hydraulic system.
  • Fig. 3 is a top plan view of the structure of Fig. 2.
  • the invention is illustrated as being incorporated in a helicopter aircraft comprising generally a body l0 mounting a lift rotor I2 which is driven by a shaft I4 by means of an engine I5 through a clutch as indicated at I6.
  • the pilot's seat is indicated at H, and the rotor is arranged to be braked by means of a brake shoe device I8 which engages upon a friction disc [9 carried by the rotor shaft M.
  • the shoe device l8 may of course be of any suitable type, such as for example a double jaw mechanism which is adapted to be actuated by means of a hydraulic piston-cylinder or diaphragm device so as to alternately release and engage in frictional relation upon the disc [9 which rotates with the rotor.
  • a novel manual control mechanism which is mounted conveniently below the seat I! as indicated generally at 29 and comprises a handle portion 22 which is arranged to be pulled upwardly to apply the brake mechanism.
  • the handle portion 22 is centrally bored to receive in bolted relation therein as indicated at 23, a pair of concentric inner and outer tubes 24-25, respectively.
  • the handle portion 22 is also formed with an enlarged annular chamber portion 26 which encircles the outer tube 25 and is arranged in fluidsealed relation therewith by means of a packing 28.
  • the casing portion 26 provides a hollow chamber which constitutes the fluid reservoir portion of the device for containing a supply of hydraulic fluid therein; the latter being maintained at a level within the reservoir such as is indicated at 29 (Fig. 2).
  • a filler plug 30 (Fig. 3) is provided in a top portion of the reservoir casing 26 for convenient replenishment of the oil supply, as needed.
  • the upper end of the handle portion 22 is centrally bored as indicated at 32 in communication with the interior of the inner tube 24, and the 3 bore 32 communicates at its upper end with a transverse groove 33 which is formed in the top surface of the handle member and is covered by a cover plate 34 so that even though the operators hand may be firmly pressed downwardly upon the handle member 22, the air vent passageway provided by the bore 32 and the groove 33 will not be covered and thereby closed off.
  • the upper end portion of the inner tube 24 is at all times in open communication with the ambient atmosphere.
  • the inner tube-121 is par-- titioned by means of a plug 36 which is riveted or otherwise fixed within the bore of; the tube 24. as indicated at 31 and function'sa'sa fluid splash baflle.
  • the bore of the tube 24 is. divided into upper and lower portions, and fluid ports 38-39 are formed through the walls ofthe tubes" 24-25, respectively, in positional alignment so as to provide for free fluid transfer between the reservoir'26 and the lower chamber'port'ion within the tube 24.
  • the outer tube 25 terminates in aringportion 50 whichslide-flts upon 2.
  • cylinder: 52 which isfixed to extend upwardly from a base member 54.
  • a valve rod 56 is also fixed to extend upwardly from the base 54 through the cylinder 52.
  • the slide ring ll is fluid-sealedrelative to the cylinder 52 asby means of an O-ring seal 59.
  • the base bracket 54 is bored as indicated at 60 in communication with the interior of. the cylinder 52, and the-cylinderwall. is ported as indicated at 62.
  • a floating valvezring 64 isdisposed. within theouter tube. 25 to abut. the lower end of the tube 2.4 and to slidably float within the tube 25 between the lower end of the tube 24 and the top end of the cylinder 52, as will be explained more fully hereinafter.
  • a fluid space-65 is provided between the tube 25 .andthe cylinder 52.
  • An O-ring device as indicated at 65 is.
  • the ring 64 is formed with a conical-valve seat portion 68 whichis arranged to engage a frusto-conical valve member which is carried at thetop-end of the rod 56.
  • the brake shoe actuator, the conduit 14, and the brake.actu ating handle device are allrfilled with hydraulic fluid, exceptv that the handle device is filled with fluid only up. to thelevelsuchsas. is indicated at 29 (Fig. 2) the ball 44 being preselected to be of such weight as to seat upon the valve disc 46 to maintain a pressure head against the hydraulic fluid column in the conduit 14 which will maintain the hydraulic fluid to flll the conduit 14 and the brake shoe actuator mechanism once the system is primed.
  • this automatic valve ball device will automaticallyadapt the unit'to changing atmospheric pressure conditions externally thereof because whenever the air pressure within the reservoir Z'oexce'edsthe atmospheric pressure'externally of the device the ball. 44 will function as a check valve to cause. adjustment of thesystem' pressure so as to maintain the desired pressurev differential, wherebythe ball 44 continues to control'the pressure head against thehydraulic system; and whenever the internal reservoir pressure fallsbelow theambient atmospheric pressuredue'to'pulling up upon the handle 22 the valve.
  • a hydraulic pressure responsive actuator comprising relatively displaceable pistoncylinder means arranged in telescopic relation and defining therebetween a fluid chamber, a closed conduit interconnecting said chamber and said hydraulic pressure responsive actuator, a fluid reservoir adjacent said chamber and arranged for communication with the latter, a check valve controlling communication between said reservoir and said chamber, and means maintaining fluid under air pressure at a preselected head within said reservoir, said means comprising a weighted ball member seated upon a perforated valve disc and disposed within an air vent conduit from said reservoir to the atmosphere externally thereof, whereby said weighted ball member controls the flow of air into and out of said reservoir and thereby determines the pressure head against said hydraulic system.
  • a control device comprising relatively displaceable piston-cylinder means arranged in telescopic relation and defining therebetween a fluid chamber disposed at a lower elevation than said actuator means, a closed conduit interconnecting said chamber and said actuator means, a fluid reservoir adjacent said chamber and arranged in communication with the latter as controlled by a check valve device, and means maintaining fluid under air pressure at a preselected head within said reservoir, said means comprising a weight member seated upon a perforated valve disc and disposed within an air vent conduit from said reservoir to the atmosphere externally thereof, whereby said weight member controls the flow of air into and out of said reservoir and thereby determines the pressure head against said hydraulic system.
  • a control device comprising relatively displaceable piston-cylinder means defining therebetween a fluid chamber, a closed conduit interconnecting said chamber and said responsive actuating means, a fluid reservoir adjacent said chamber and arranged in communication with the latter as controlled by a check valve device, and means maintaining fluid under air pressure at a preselected head within said reservoir, said means comprising a weight member seated upon a perforated valve disc and disposed within an air vent conduit from said reservoir to the atmosphere externally thereof, whereby said weight member controls the flow of air into and out of said reservoir and thereby determines the pressure head against said hydraulic system.
  • a hydraulic pressureresponsive actuator comprising relatively displaceable pistoncylinder means arranged in telescopic relation and defining therebetween a fluid chamber disposed at an elevation below the elevation of said actuator, a closed conduit interconnecting said chamber and said hydraulic pressure-responsive actuator, a fluid reservoir adjacent said chamber and arranged for communication with the latter, a check valve controlling communication between said reservoir and said chamber, and means maintaining fluid under air pressure at a preselected head within said reservoir, said means comprising a weighted ball member seated upon a perforated valve disc and disposed within an air vent conduit from said reservoir to the atmosphere externally thereof, whereby said weighted ball member controls the flow of air into and out of said reservoir and thereby determines the pressure head against said hydraulic system.
  • a hydraulic pressure responsive actuating means comprising a hydraulic jack disposed at an elevation below said pressure responsive actuating means and defining a fluid chamber, a closed conduit interconnecting said chamber and said responsive actuating means, a fluid reservoir adjacent said chamber and arranged in communication with the latter as controlled by a check valve device, and means maintaining fluid under air pressure at a pre-selected head within said reservoir, said means comprising a weight member seated upon a perforated valve disc and disposed within an air vent conduit (from said reservoir to the atmosphere externally thereof, whereby said weight member controls the flow of air into and out of said reservoir and thereby determines the pressure head against said hydraulic system.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Braking Arrangements (AREA)

Description

June 17, 1952 J. w. WHEELER HYDRAULIC BRAKE ACTUATOR FOR HELICOPTER ROTORS Filed Jan. 3, 1950 INVENTOR Ja/m h! h/fiee/e/ M ATTORN EYS Patented June 17, 1952 HYDRAULIC BRAKE ACTUATOR FOR. HELICOPTER ROTORS John W. Wheeler, Grand Island, N. Y., assignor to Bell Aircraft Corporation, Wheatfield, N. Y.
Application January 3, 1950, Serial No. 136,445
6 Claims. (01. 60-54.5)
Thisinvention relates to helicopter aircraft, and more particularly to an improved hydraulic brake device for helicopter rotors and the like wherein the brake actuator mechanism is necessarily at a higher elevation than the control piston-cylinder mechanism.
Whereas, it is presently known to be desirable to provide in helicopter type aircraft some suitable brake device for halting coasting rotation of the helicopter rotor subsequent to landin of the aircraft and disengagement of the rotorengine clutch; it has been noted that such brake devices must be constructed so as to obtain uniform braking effects under various conditions of operation in order to avoid unpredictable reactions upon the grounded aircraft. Furthermore, it has been noted that prior type hydraulic brake systems for the purposes referred to herein are productive of highly variable braking effects because of the tendencies to develop cavitation in the hydraulic line when the brake actuator piston-cylinder is at an elevation above the control piston-cylinder; and also as a result of changing ambient atmospheric pressure conditions, as when operating the aircraft on landing fields at different elevations above sea level.
Also, it has been noted that temperature changes result in expansion-contraction of the oil in the hydraulic system and require that the oil level in the reservoir change correspondingly; and therefor it is one of the objects of the present invention to provide an improved rotor braking system for helicopter aircraft and the like of the manually controlled hydraulic actuated type which will provide uniform braking effects under varying conditions as aforesaid.
Another object of the invention is to provide an improved braking system of the character aforesaid which automatically maintains a predetermined constant pressure differential in the braking system relative to the ambient atmosphere in spite of variations in the atmospheric pressure.
Another object of the invention is to provide an improved braking system of the character aforesaid which operates automatically to maintain the hydraulic line between the control piston and the brake actuator filled with hydraulic fluid and to prevent cavitation therein, whereby pumping of the control piston is unnecessary to condition the system for effective operation, and whereby uniformly short stroke operation of the control piston will provide effective brake actuation.
Another object of the invention is to provide an improved braking system embodying the features aforesaid and which is of relatively simple and inexpensive yet rugged construction.
Other objects and advantages of the invention will appear from the specification hereinafter.
In the drawing:
Fig. 1 is a fragmentary side elevation of a helicopter aircraft embodying a rotor brake system of the invention;
Fig. 2 is a fragmentary vertical section throug the manual control portion of the hydraulic system; and
Fig. 3 is a top plan view of the structure of Fig. 2.
As shown in Fig. 1, the invention is illustrated as being incorporated in a helicopter aircraft comprising generally a body l0 mounting a lift rotor I2 which is driven by a shaft I4 by means of an engine I5 through a clutch as indicated at I6. The pilot's seat is indicated at H, and the rotor is arranged to be braked by means of a brake shoe device I8 which engages upon a friction disc [9 carried by the rotor shaft M. The shoe device l8 may of course be of any suitable type, such as for example a double jaw mechanism which is adapted to be actuated by means of a hydraulic piston-cylinder or diaphragm device so as to alternately release and engage in frictional relation upon the disc [9 which rotates with the rotor.
To control the brake shoe device 18 I provide a novel manual control mechanism which is mounted conveniently below the seat I! as indicated generally at 29 and comprises a handle portion 22 which is arranged to be pulled upwardly to apply the brake mechanism. The handle portion 22 is centrally bored to receive in bolted relation therein as indicated at 23, a pair of concentric inner and outer tubes 24-25, respectively. The handle portion 22 is also formed with an enlarged annular chamber portion 26 which encircles the outer tube 25 and is arranged in fluidsealed relation therewith by means of a packing 28. Thus, the casing portion 26 provides a hollow chamber which constitutes the fluid reservoir portion of the device for containing a supply of hydraulic fluid therein; the latter being maintained at a level within the reservoir such as is indicated at 29 (Fig. 2). A filler plug 30 (Fig. 3) is provided in a top portion of the reservoir casing 26 for convenient replenishment of the oil supply, as needed.
The upper end of the handle portion 22 is centrally bored as indicated at 32 in communication with the interior of the inner tube 24, and the 3 bore 32 communicates at its upper end with a transverse groove 33 which is formed in the top surface of the handle member and is covered by a cover plate 34 so that even though the operators hand may be firmly pressed downwardly upon the handle member 22, the air vent passageway provided by the bore 32 and the groove 33 will not be covered and thereby closed off. Thus, it will be understood that the upper end portion of the inner tube 24 is at all times in open communication with the ambient atmosphere.
At about the elevation of the fluid level. 29:
within the reservoir 26, the inner tube-121 is par-- titioned by means of a plug 36 which is riveted or otherwise fixed within the bore of; the tube 24. as indicated at 31 and function'sa'sa fluid splash baflle. Thus, the bore of the tube 24 is. divided into upper and lower portions, and fluid ports 38-39 are formed through the walls ofthe tubes" 24-25, respectively, in positional alignment so as to provide for free fluid transfer between the reservoir'26 and the lower chamber'port'ion within the tube 24. Similarly, ports 48-41 formed through the walls of the tubes 2425 above the position of the plug 36 intercommunicate the air space Within the reservoir 26 and the upper bore portion of the tube-24l Above the elevation of the port 40 in the wall of the tube 24, I provide an automatic pressure regulator device comprising a plug 42 which is centrally bored to accommodate in free floating position therein a steel ball 44 which is arranged to rest upon a centrally bored rubber disc 46 which is in turn supported by a perforated metal cone-41 which issnap-fltted into the lower flanged end portion of the plug 42. Air passageways 48 are provided through the body of the plug 42 above the-position or the valve disc 46 so that the airchamber portion within the casing 26 is in communication withthe atmosphere externally of the device by means of' the channel 33, the bore=32, the passageways-48, and the ports 40-4 as controlled by operation of the valve ball 44 relative to the opening through the valve disc At its lower end the outer tube 25 terminates in aringportion 50 whichslide-flts upon 2. cylinder: 52which isfixed to extend upwardly from a base member 54. A valve rod 56 is also fixed to extend upwardly from the base 54 through the cylinder 52. The slide ring llis fluid-sealedrelative to the cylinder 52 asby means of an O-ring seal 59. The base bracket 54 is bored as indicated at 60 in communication with the interior of. the cylinder 52, and the-cylinderwall. is ported as indicated at 62. A floating valvezring 64 isdisposed. within theouter tube. 25 to abut. the lower end of the tube 2.4 and to slidably float within the tube 25 between the lower end of the tube 24 and the top end of the cylinder 52, as will be explained more fully hereinafter. Thus, a fluid space-65is provided between the tube 25 .andthe cylinder 52. An O-ring device as indicated at 65 is. arranged to fluid-seal the ring 64 relative to the tube 25;.andthe ring 64 is formed with a conical-valve seat portion 68 whichis arranged to engage a frusto-conical valve member which is carried at thetop-end of the rod 56.
The base: bracket 54 extendsasindicatedat l2 into=connection with a conduit 14 (Fig. '1) which leads to the brake shoe mechanism IS. The brake shoe actuator, the conduit 14, and the brake.actu ating handle device are allrfilled with hydraulic fluid, exceptv that the handle device is filled with fluid only up. to thelevelsuchsas. is indicated at 29 (Fig. 2) the ball 44 being preselected to be of such weight as to seat upon the valve disc 46 to maintain a pressure head against the hydraulic fluid column in the conduit 14 which will maintain the hydraulic fluid to flll the conduit 14 and the brake shoe actuator mechanism once the system is primed. Upon manual pulling of thehandle 22' upwardly the reservoir and the outer tube will be thereby'displaced upwardly relative to the cylinder 52 while the valve rod 56 maintains the valve ring 64 at the elevation thereof shownin Fig. 2. Consequently, such upwardidisplacement of the outer tube 25 will cause the distance between the lower ring and the fi'oatin'gring, 64': to shorten, whereby the fluid within the space will be forced through the ports. 62 and-thence downwardly through the interior. of the cylinder 52 and through the bore 60 into the conduit 14 in such manner as to thereby apply increased pressure through the conduit against the. brake shoe actuator mechanism, thereby causing the brake: to be applied to the rotor disc I'll. Then, upon release of the handle 22; 'theflat'ter will fsimply settle down again tolts normal inoperativeposition; the" fluid previously forced up into the brake actuator now finding return through the conduit into the enlarging space within thecontrol handle device;
Ina'smuch as'th'e'ring: 64 is:frec tofloat within the tube 25': betweenipositionsof-abutment against the bottom end of the tube 24 and the upper endof the cylinder 52,. it. will be: appreciated. that whenever the device is in condition ofrepose the valve. surfaces EL -7.9 will be relatively free to permit settling of fluid from the: reservoir through the. ports 36-39 and into thecylinder space 55; thereby at all times maintaining the operative: systemin .iull supply of fluid. Also, it will be appreciated that, as. stated hereinabove, the preselected weight of the valve ball 44 and the size of the central hole. in the disc 46 will determine. the pressure head which will apply against the air within the chamber 26 above the fluid level: therein; and consequently, the pressure head through the: hydraulic system against the brake shoe'actuator. Also,. it will be appreciated that this automatic valve ball device will automaticallyadapt the unit'to changing atmospheric pressure conditions externally thereof because whenever the air pressure within the reservoir Z'oexce'edsthe atmospheric pressure'externally of the device the ball. 44 will function as a check valve to cause. adjustment of thesystem' pressure so as to maintain the desired pressurev differential, wherebythe ball 44 continues to control'the pressure head against thehydraulic system; and whenever the internal reservoir pressure fallsbelow theambient atmospheric pressuredue'to'pulling up upon the handle 22 the valve. seat device 46'operates-to permit entry of air into the reser- Hence, the system of the invention is at all times maintained in fluid-charged and optimum condition for operation under constant pressure head eflects in. spite of temperature or ambient pressure variations, wherebythe aircraft operator may without undue attention to the device employ the brake control mechanism to obtain uniformly predictable braking effects upon the coasting rotor. It will of course be appreciated'that although only one dorm of the invention has been shown and described in detail it will be apparent to those skilled in the art that the invention is not so limited but that various changes may be made therein without departing from the spirit of the invention or the scope of the appended claims.
I claim:
1. In combination, a hydraulic pressure responsive actuator, a hydraulic control device comprising relatively displaceable pistoncylinder means arranged in telescopic relation and defining therebetween a fluid chamber, a closed conduit interconnecting said chamber and said hydraulic pressure responsive actuator, a fluid reservoir adjacent said chamber and arranged for communication with the latter, a check valve controlling communication between said reservoir and said chamber, and means maintaining fluid under air pressure at a preselected head within said reservoir, said means comprising a weighted ball member seated upon a perforated valve disc and disposed within an air vent conduit from said reservoir to the atmosphere externally thereof, whereby said weighted ball member controls the flow of air into and out of said reservoir and thereby determines the pressure head against said hydraulic system.
2. In combination hydraulic pressure responsive actuator means, a control device comprising relatively displaceable piston-cylinder means arranged in telescopic relation and defining therebetween a fluid chamber disposed at a lower elevation than said actuator means, a closed conduit interconnecting said chamber and said actuator means, a fluid reservoir adjacent said chamber and arranged in communication with the latter as controlled by a check valve device, and means maintaining fluid under air pressure at a preselected head within said reservoir, said means comprising a weight member seated upon a perforated valve disc and disposed within an air vent conduit from said reservoir to the atmosphere externally thereof, whereby said weight member controls the flow of air into and out of said reservoir and thereby determines the pressure head against said hydraulic system.
3. In combination, hydraulic pressure responsive actuating means, a control device comprising relatively displaceable piston-cylinder means defining therebetween a fluid chamber, a closed conduit interconnecting said chamber and said responsive actuating means, a fluid reservoir adjacent said chamber and arranged in communication with the latter as controlled by a check valve device, and means maintaining fluid under air pressure at a preselected head within said reservoir, said means comprising a weight member seated upon a perforated valve disc and disposed within an air vent conduit from said reservoir to the atmosphere externally thereof, whereby said weight member controls the flow of air into and out of said reservoir and thereby determines the pressure head against said hydraulic system.
4. In combination, a hydraulic pressureresponsive actuator, a hydraulic control device comprising relatively displaceable pistoncylinder means arranged in telescopic relation and defining therebetween a fluid chamber disposed at an elevation below the elevation of said actuator, a closed conduit interconnecting said chamber and said hydraulic pressure-responsive actuator, a fluid reservoir adjacent said chamber and arranged for communication with the latter, a check valve controlling communication between said reservoir and said chamber, and means maintaining fluid under air pressure at a preselected head within said reservoir, said means comprising a weighted ball member seated upon a perforated valve disc and disposed within an air vent conduit from said reservoir to the atmosphere externally thereof, whereby said weighted ball member controls the flow of air into and out of said reservoir and thereby determines the pressure head against said hydraulic system.
5. In combination, a hydraulic pressure responsive actuator, a control device comprising a hydraulic jack disposed at an elevation below said actuator and defining a fluid chamber, a
closed conduit interconnecting said chamber and said actuator, a fluid reservoir adjacent said chamber andarranged in communication with the latter as controlled by a check valve device, and means maintaining fluid under air pressure at a pro-selected head within said reservoir, said means comprising a weighted ball member seated upon a perforated valve disc and disposed within an air vent conduit from said reservoir to the atmosphere externally therof, whereby said weighted ball member controls the flow of air into and out of said reservoir and thereby determines the pressure head against said hydraulic system.
6. In combination, a hydraulic pressure responsive actuating means, a control means comprising a hydraulic jack disposed at an elevation below said pressure responsive actuating means and defining a fluid chamber, a closed conduit interconnecting said chamber and said responsive actuating means, a fluid reservoir adjacent said chamber and arranged in communication with the latter as controlled by a check valve device, and means maintaining fluid under air pressure at a pre-selected head within said reservoir, said means comprising a weight member seated upon a perforated valve disc and disposed within an air vent conduit (from said reservoir to the atmosphere externally thereof, whereby said weight member controls the flow of air into and out of said reservoir and thereby determines the pressure head against said hydraulic system.
JOHN W. WHEELER.
REFERENCES CITED The following references are of record in the file of this patent:
UNITED STATES PATENTS
US136445A 1950-01-03 1950-01-03 Hydraulic brake actuator for helicopter rotors Expired - Lifetime US2600715A (en)

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Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3451644A (en) * 1965-04-08 1969-06-24 Marchetti Soc Charles Vertical or short take-off aerodyne of high translation speed
US5855471A (en) * 1997-06-17 1999-01-05 Sikorsky Aircraft Corporation Helicopter rotor brake assembly
US6077042A (en) * 1997-08-01 2000-06-20 Finmeccanica S.P.A. Helicopter rotor brake
US20050133314A1 (en) * 2003-12-19 2005-06-23 Eurocopter Brake device for the rotor of a helicopter or the like, associating a main brake mechanism having a disk and a secondary brake mechanism for use in strong wind

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1999737A (en) * 1931-06-19 1935-04-30 Autogiro Co Of America Aircraft having sustaining rotors
US2115174A (en) * 1933-10-06 1938-04-26 Ludwig A Majneri Fluid pressure control mechanism
US2141091A (en) * 1934-09-10 1938-12-20 Heron Crosman J Means for stopping rotation of propellers
US2197126A (en) * 1939-03-18 1940-04-16 Wagner Electric Corp Braking system
GB549333A (en) * 1941-04-11 1942-11-17 Rover Co Ltd Improvements relating to pumps for hydraulic vehicle brake systems
US2344299A (en) * 1942-03-28 1944-03-14 Arthur Wilde Hydraulic actuating mechanism

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1999737A (en) * 1931-06-19 1935-04-30 Autogiro Co Of America Aircraft having sustaining rotors
US2115174A (en) * 1933-10-06 1938-04-26 Ludwig A Majneri Fluid pressure control mechanism
US2141091A (en) * 1934-09-10 1938-12-20 Heron Crosman J Means for stopping rotation of propellers
US2197126A (en) * 1939-03-18 1940-04-16 Wagner Electric Corp Braking system
GB549333A (en) * 1941-04-11 1942-11-17 Rover Co Ltd Improvements relating to pumps for hydraulic vehicle brake systems
US2344299A (en) * 1942-03-28 1944-03-14 Arthur Wilde Hydraulic actuating mechanism

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3451644A (en) * 1965-04-08 1969-06-24 Marchetti Soc Charles Vertical or short take-off aerodyne of high translation speed
US5855471A (en) * 1997-06-17 1999-01-05 Sikorsky Aircraft Corporation Helicopter rotor brake assembly
US6077042A (en) * 1997-08-01 2000-06-20 Finmeccanica S.P.A. Helicopter rotor brake
US20050133314A1 (en) * 2003-12-19 2005-06-23 Eurocopter Brake device for the rotor of a helicopter or the like, associating a main brake mechanism having a disk and a secondary brake mechanism for use in strong wind
FR2864027A1 (en) * 2003-12-19 2005-06-24 Eurocopter France Helicopter rotor braking device, has secondary braking mechanism including lever that is operated to move finger against spring unit, where finger exerts pressure against another lever of primary braking mechanism to move yoke
US6991072B2 (en) 2003-12-19 2006-01-31 Eurocopter Brake device for the rotor of a helicopter or the like, associating a main brake mechanism having a disk and a secondary brake mechanism for use in strong wind

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